SAE AMS 2175 : 2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CASTINGS, CLASSIFICATION AND INSPECTION OF
Available format(s)
Hardcopy , PDF
Superseded date
02-09-2019
Superseded by
Language(s)
English
Published date
01-01-2010
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Sets up non-destructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castings.
| Committee |
AMS-B
|
| DevelopmentNote |
Supersedes SAE AMS STD 2175 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE AMS5349E | Steel, Corrosion-Resistant, Investment Castings 13Cr Free Machining; Hardened and Tempered |
| SAE AMS5346C | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb (Nb) - 2.8Cu Solution and Precipitation Heat Treated (H925) 180 ksi (1241 MPa) Tensile Strength (15-5) |
| SAE AMS4992B | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
| SAE AMS 2694 : 2013 | IN-PROCESS WELDING OF CASTINGS |
| SAE AMSA21180C | Aluminum-Alloy Castings, High Strength |
| MIL-DTL-23599 Revision C:2017 | Hook, Rescue |
| SAE AMS 5396 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 65NI - 28MO - 5.5FE - 0.40V (N-12MV), AS-CAST |
| SAE AMS4284K | Aluminum Alloy Castings, Permanent Mold 7.0Si - 0.30Mg (356.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS4217J | Aluminum Alloy, Castings 7.0Si - 0.32Mg (356.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS4223E | Aluminum Alloy, Castings 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T4) Solution Heat Treated and Naturally Aged |
| SAE AMS4241E | Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled |
| SAE AMS 5390 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 47.5NI - 22CR - 1.5CO - 9MO - 0.60W - 18.5FE (N-12MV) AS-CAST |
| SAE AMS4280J | Aluminum Alloy Castings, Permanent Mold 5.0Si - 1.2Cu - 0.5Mg (355.0-T71) Solution Heat Treated and Overaged |
| SAE AMS 5401 : 2004 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 62NI - 21.5CR - 9.0MO - 3.6CB (NB), VACUUM MELTED, VACUUM CAST, AS CAST |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-87104 Revision C:2014 | COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS5356D | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution and Precipitation Heat Treated (H1100) 130 ksi (896 MPa) Tensile Strength |
| SAE AMS5350K | Steel, Corrosion and Moderate Heat-Resistant, Investment Castings 12.5Cr (410) Hardened and Tempered |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| SAE AMS4286F | Aluminum Alloy Castings, Permanent Mold 7.0Si - 0.32Mg (356.0-T51) As-Cast then Precipitation Heat Treated |
| SAE AMS5366E | Steel, Corrosion and Heat-Resistant, Investment Castings 25Cr - 20Ni (CK-20) As-Cast |
| MIL-DTL-16377 Revision J:2014 | Fixtures, Lighting; and Associated Parts; Shipboard Use, General Specification for |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE AMS4235C | Aluminum Alloy Castings 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0-T7) Solution and Precipitation Heat Treated |
| SAE AMS4290M | Aluminum Alloy, Die Castings 9.5Si - 0.50Mg (360.0-F) As Cast |
| SAE AMS 4484 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 9.0AL - 2.0ZN (AZ92A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS4406A | Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated |
| SAE AMS4210K | Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat Treated |
| SAE AMS 5399 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION HEAT TREATED |
| SAE AMS 4985 : 2014 | TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED |
| SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
| SAE AMS4873F | Aluminum Bronze Alloy, Sand Castings 85Cu - 11Al - 3.6Fe Solution Heat Treated and Tempered |
| SAE AMS5383E | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb(Nb) - 0.90Ti - 0.60Al - 18Fe Vacuum Melted Homogenization and Solution Heat Treated |
| SAE AMS 5377 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 73NI - 12CR - 4.5MO - 2.0CB - 0.70TI - 0.05C - 6.0AL - 0.010 - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS 4892 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, AS CAST |
| SAE AMS5347B | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb (Nb) - 2.8Cu Solution and Precipitation Heat Treated (H1000) 150 ksi (1034 MPa) Tensile Strength (15-5) |
| SAE AMS 4483 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 10AL (AM100A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5356 : 2016 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1100), 130 KSI (896 MPA) TENSILE STRENGTH |
| SAE AMS5387E | Alloy, Corrosion and Heat Resistant, Investment Castings 60Co - 29Cr - 4.5W As Cast |
| SAE AMS5342E | Steel, Corrosion-Resistant, Investment Castings 16Cr - 4.1Ni - 0.28Cb (Nb) - 3.2Cu Homogenization, Solution, and Precipitation Heat Treated (H1100) 130 ksi (896 MPa) Tensile Strength (17-4) |
| SAE AMS4285F | Aluminum Alloy Castings, Centrifugal 7.0Si - 0.30Mg (356.0-T6) Solution and Precipitation Heat Treated |
| MIL-HDBK-115 Revision C:2016 | U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| SAE AMS4249A | Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) |
| MIL-DTL-6396 Revision F:2008 | TANKS, FUEL, OIL, COOLING FLUIDS, INTERNAL, REMOVABLE NON-SELF-SEALING |
| SAE AMS5344F | Steel, Corrosion-Resistant, Investment Castings 16Cr - 4.1Ni - 0.28Cb - 3.2Cu Homogenization, Solution, and Precipitation Heat Treated (H900) 180 ksi (1241 MPa) Tensile Strength (17-4) |
| SAE AMS5412A | Steel Castings, Vacuum Melted, Vacuum Cast, Investment, Corrosion-Resistant 13Cr - 8.0Ni - 2.2Mo - 1.1Al (195 ksi (1344 MPa) Tensile Strength (Condition H1000) Homogenized, Solution, and Precipitation Heat Treated |
| SAE AMS4439G | Magnesium Alloy Castings 4.2Zn - 1.2 Rare Earths - 0.7Zr (ZE41A-T5) Precipitation Heat Treated |
| SAE AMS5343E | Steel, Corrosion-Resistant, Investment Castings 16Cr - 4.1Ni - 0.28Cb (Nb) - 3.2Cu Homogenization, Solution, and Precipitation Heat Treated (H1000) 150 ksi (1034 MPa) Tensile Strength (17-4) |
| SAE AMS 5338 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.35 - 0.45C) (4140 MOD), NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS4482 | Cast Aluminum Alloy Composite 4.6 Cu – 3.4Ti – 1.4B – 0.75Ag – 0.27Mg (A205.0/TiB2/3p-T7P) Sand Cast, Solution and Precipitation Heat Treated |
| SAE AMS4225E | Aluminum Alloy, Heat-Resistant, Castings 5.0Cu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T6) Solution Heat Treated and Precipitation Heat Treated |
| SAE AMS 5388 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 53.3NI - 16.5CR - 17MO - 4.5W - 5.8FE - 0.40V (CW-12MW), AS-CAST |
| SAE AMS4212L | Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS5400C | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution and Precipitation Heat Treated (H935) 170 ksi (1172 MPa) Tensile Strength |
| SAE AMS4443H | Magnesium Alloy, Sand Castings 4.5Zn - 0.75Zr (ZK51A-T5) Precipitation Heat Treated |
| SAE AMS 5385 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 62MO - 27CR - 2.8NI - 5.5MO, AS-CAST |
| SAE AMS 7918 : 2016 | BERYLLIUM ALUMINUM ALLOY INVESTMENT CASTINGS, 64.9BE - 30AL - 3AG - 1CO - 0.75GE, AS CAST |
| SAE AMS 5410 : 2017 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.85CB (NB) - 3.4TI - 1.8TA - 3.4AL - 0.010B - 0.05ZR, VACUUM MELTED, VACUUM CAST AS CAST, OR SOLUTION TREATED, OR SOLUTION AND PRECIPITATION HARDENED |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA MSFC STD 3716 : 2017 | STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| MIL-PRF-21480 Revision B:2010 | Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| SAE AMS4219F | Aluminum Alloy Castings 7.0Si - 0.55Mg - 0.12Ti - 0.06Be (A357.0 T6) Solution and Precipitation Heat Treated |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| SAE AMS4214J | Castings, Aluminum Alloy Sand 5.0Si - 1.2Cu - 0.50Mg (355.0-T71) Solution Heat Treated and Overaged |
| SAE AMS4261G | Aluminum Alloy Castings, Investment 7.0Si - 0.32Mg (356.0-T51) Precipitation Heat Treated |
| MIL-DTL-2036 Revision E:2014 | ENCLOSURES FOR ELECTRIC AND ELECTRONIC EQUIPMENT, NAVAL SHIPBOARD |
| SAE AMS5368D | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.0Ni - 2.3Mo - 0.09N Solution Heat Treated |
| SAE AMS 5391 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 73NI - 0.14C - 13CR - 4.5MO - 2.3CB (NB) - 0.75TI - 6.0AL - 0.010B - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS 4893 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, SOLUTION TREATED |
| SAE AMS5334H | Steel, Investment Castings 0.50Cr - 0.55Ni - 0.20Mo (0.25 - 0.35C) (SAE 8630 Mod) Normalized and Tempered |
| ASTM E 1417/E1417M : 2016 : REDLINE | Standard Practice for Liquid Penetrant Testing |
| SAE AMS4236D | Aluminum Alloy Castings 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0-T4) Solution Heat Treated and Naturally Aged |
| SAE AMS4229G | Aluminum Alloy Castings, High Strength 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T7) Solution Heat Treated and Overaged |
| SAE AMS4452E | Magnesium Alloy, Investment Castings 8.7Al - 0.70Zn - 0.22Mn (AZ91C-T6) Solution and Precipitation Heat Treated |
| SAE AMS4215H | Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (C355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS4453F | Magnesium Alloy, Investment Castings 9.0Al - 2.0Zn (AZ92A-T6) Solution and Precipitation Heat Treated |
| SAE AMS5357D | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution Heat Treated, Precipitation Hardenable |
| SAE AMS5339G | Steel, Maraging, Investment Castings 17Ni - 10Co - 4.6Mo - 0.30Ti - 0.06Al Vacuum Melted Homogenized, Overaged, and Solution Heat Treated |
| SAE AMS4281G | Aluminum Alloy Castings, Permanent Mold 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS5352F | Steel, Corrosion-Resistant, Investment Castings 17Cr - 0.55Mo (0.95 - 1.20C) Annealed |
| SAE AMS4455G | Magnesium Alloy, Investment Castings 10Al (AM100A-T6) Solution and Precipitation Heat Treated |
| SAE AMS 5333 : 2017 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.25MO (0.11 - 0.17C) (SAE 8615), NORMALIZED |
| SAE AMS 5350 : 2017 | STEEL, CORROSION AND MODERATE HEAT-RESISTANT, INVESTMENT CASTINGS, 12.5CR (410), HARDENED AND TEMPERED |
| SAE AMS 5336 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.25 - 0.35C) (4130 MOD) NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS5360F | Steel, Corrosion and Heat-Resistant, Investment Castings 17Cr - 13Ni - 1.9Mo Solution Heat Treated |
| SAE AMS 5380 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 50.5CO - 26CR - 15NI - 6.0MO, AS-CAST |
| SAE AMS5337E : 2017 | STEEL, MARAGING, INVESTMENT CASTINGS, 18.5NI - 9.0CO - 5.0MO - 0.70TI - 0.12AL, VACUUM MELTED, HOMOGENIZED, OVERAGED, AND SOLUTION HEAT TREATED |
| SAE AMS5354F | Steel, Corrosion and Heat Resistant, Investment Castings 13Cr - 2.0Ni - 3.0W Hardened and Tempered to 32 – 38 HRC |
| SAE AMS5364C | Steel, Corrosion and Heat-Resistant, Investment Castings 19.5Cr - 10.5Ni - 0.65Cb (CF-8C) Solution Heat Treated |
| SAE AMS4471A | Cast Aluminum Alloy Composite 4.6Cu - 3.4Ti - 1.4B - 0.75Ag - 0.27Mg (205.0/TiB2/3p-T7P) Investment Cast, Solution and Precipitation Heat Treated |
| SAE AMS5402C | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) As Cast |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMS5353E | Steel, Corrosion-Resistant, Investment Castings 16Cr - 1.8Ni - 0.08N As Cast |
| SAE AMS4242C | Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged |
| ASTM F 3318 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Specification for AlSi10Mg with Powder Bed Fusion – Laser Beam |
| SAE AMS5401C | Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) Vacuum Melted, Vacuum Cast As Cast |
| SAE AMS4992D | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
| ASTM E 446 : 2015 : REDLINE | Standard Reference Radiographs for Steel Castings Up to 2 in. (50.8 mm) in Thickness |
| ASTM E 186 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (2 to 4<fraction><num>1</num><den>2</den></fraction > in. (50.8 to 114 mm)) Steel Castings |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| ASTM E 155 : 2015 : REDLINE | Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings |
| ASTM E 1320 : 2015 : REDLINE | Standard Reference Radiographs for Titanium Castings |
| ASTM E 1255 : 2016 : REDLINE | Standard Practice for Radioscopy |
| ASTM E 2104 : 2015 : REDLINE | Standard Practice for Radiographic Examination of Advanced Aero and Turbine Materials and Components |
| ASTM E 192 : 2015 : REDLINE | Standard Reference Radiographs of Investment Steel Castings for Aerospace Applications |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| ASTM E 272 : 2015 : REDLINE | Standard Reference Radiographs for High-Strength Copper-Base and Nickel-Copper Alloy Castings |
| ASTM E 280 : 2015 : REDLINE | Standard Reference Radiographs for Heavy-Walled (4<fraction><num>1</num><den>2</den></fraction > to 12 in. (114 to 305 mm)) Steel Castings |
| ASTM E 310 : 2015 : REDLINE | Standard Reference Radiographs for Tin Bronze Castings |
| ASTM E 2422 : 2017 : REDLINE | Standard Digital Reference Images for Inspection of Aluminum Castings |
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